| 摘要 |
PCT No. PCT/GB92/00994 Sec. 371 Date Jan. 21, 1994 Sec. 102(e) Date Jan. 21, 1994 PCT Filed Jun. 3, 1992 PCT Pub. No. WO93/02920 PCT Pub. Date Feb. 18, 1993.A gas turbine engine nacelle assembly (10) comprises a pylon (13) for mounting the assembly on an aircraft, a nacelle (11) and a gas turbine engine (12) enclosed within the nacelle (11). Part (15) of the nacelle (11) is structurally integral with the pylon (13) and has the remainder of the nacelle (11) attached to it. The nacelle part (15) additionally provides at least partial support for the gas turbine engine (12). The arrangement provides weight savings.
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